#ifndef BAROALT_H_
#define BAROALT_H_

 __BEGIN_DECLS
 
 /**
  * Calculate baro altitude
  *
  * @param total_pressure pressure inside the pitot/prandtl tube
  * @param static_pressure pressure at the side of the tube/airplane
  * @return indicated airspeed in m/s
  */
 __EXPORT float calc_baroalt(double static_pressure, double base_pressure);
 
__END_DECLS

#endif
